Investigation of Inlet Guide Vane Wakes in a F109 Turbofan Engine with and without Flow Control
A series of experiments were conducted in a F109 turbofan engine to investigate the unsteady wake profiles of an Inlet Guide Vane (IGV) at a typical spacing to the downstream fan at subsonic and transonic relative blade velocities. The sharp trailing-edge vanes were designed to produce a wake profi...
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Virginia Tech
2014
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Online Access: | http://hdl.handle.net/10919/28833 http://scholar.lib.vt.edu/theses/available/etd-08312000-14560008/ |